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    • 62. 发明申请
    • Magnet retaining arrangement
    • 磁铁保持布置
    • US20070290564A1
    • 2007-12-20
    • US11805686
    • 2007-05-24
    • Paul Clark
    • Paul Clark
    • H02K21/12H02K1/27
    • H02K1/278H02K7/1838
    • The present invention provides a permanent magnet rotor arrangement that is particularly suitable for low-speed large-diameter electrical generators. The arrangement includes a rotor 2 having a radially outer rim 4. A circumferential array of magnet carriers 12 is affixed to the outer rim 4 of the rotor and have a radially outer surface. An inverted U-shaped pole piece retainer 18 made of non-magnetic material such as stainless steel is affixed to each magnet carrier 12 and is formed with an axially extending channel. At least one pole piece 16 made of a magnetic material such as steel is located adjacent to the radially outer surface of each magnet carrier 12 and in the channel formed in its associated pole piece retainer 18.
    • 本发明提供一种特别适用于低速大直径发电机的永磁转子装置。 该装置包括具有径向外缘4的转子2.磁体支架12的圆周阵列固定到转子的外缘4并具有径向外表面。 由非磁性材料(例如不锈钢)制成的倒U形极片保持器18固定到每个磁体托架12上并形成有轴向延伸的通道。 由诸如钢等磁性材料制成的至少一个极片16位于每个磁体支架12的径向外表面附近以及形成在其相关联的极片保持器18中的通道中。
    • 63. 发明申请
    • Folding retractable protective dome for space vehicle equipment
    • 用于空间车辆设备的可折叠保护罩
    • US20060102796A1
    • 2006-05-18
    • US10970472
    • 2004-10-20
    • Paul ClarkRoss Messinger
    • Paul ClarkRoss Messinger
    • B64G1/52
    • B64G1/56B64G1/58
    • A folding, retractable dome for protecting a feature, such as a docking mechanism, a hatch or other equipment at an exterior surface of a space vehicle, includes a plurality of arcuate ribs, each having opposite ends respectively pinioned at opposite sides of the feature at the surface of the vehicle for rotational movement about an axis of rotation extending through the opposite ends and through an arcuate path of revolution extending over the feature, and a flexible cover attached to each of the ribs such that, in a deployed configuration of the dome, in which adjacent ribs are rotated apart from each other at a maximum relative angle therebetween, the cover is stretched generally tangentially between the adjacent ribs to form a generally arcuate shield over the feature, and in a retracted position of the dome, in which adjacent ribs are rotated together at a minimum relative angle therebetween, the cover is collapsed to define folded pleats between the adjacent ribs.
    • 用于保护空间车辆外表面处的特征(例如对接机构,舱口或其他设备)的折叠式伸缩式圆顶包括多个弧形肋,每个弧形肋具有分别在该特征的相对侧处的相对端 所述车辆的表面围绕旋转轴线旋转延伸,所述旋转轴线延伸穿过所述相对端并且穿过所述特征部分延伸的弧形路径,以及附接到每个所述肋部的柔性盖,使得在所述圆顶的展开构造中 ,其中相邻的肋以其最大相对角度彼此分开地旋转,所述盖大致相切地在相邻的肋之间被拉伸,以在所述特征上形成大致弧形的屏蔽,并且在所述圆顶的缩回位置中相邻 肋骨之间以最小相对角度一起旋转,盖子被折叠以在相邻的肋条之间限定折叠褶皱。
    • 64. 发明申请
    • Retractable protective dome for space vehicle equipment
    • 空间车辆设备伸缩保护球
    • US20060081343A1
    • 2006-04-20
    • US10969829
    • 2004-10-20
    • Paul ClarkRoss Messinger
    • Paul ClarkRoss Messinger
    • E06B3/12
    • B64G1/56B64G1/54B64G1/58E06B3/92
    • A retractable rigid dome for protecting a feature, such as a docking mechanism, a hatch or other equipment on an exterior surface of a space vehicle, includes a plurality of rigid arcuate segments, each having opposite ends respectively pinioned at opposite sides of the feature at about the surface of the vehicle for rotational movement about an axis of rotation extending through the opposite ends thereof and through an arcuate path of rotation extending over the feature. The radial sizes of the segments are staggered such that, in a fully deployed position of the dome, in which adjacent segments are rotated apart from each other at a maximum relative angle therebetween, the segments combine to form an arcuate shield over the feature, and in a retracted position of the dome, in which adjacent segments are rotated together at a common angle relative to the surface of the vehicle, the segments are nested in radial alignment with each other.
    • 用于保护空间车辆的外表面上的诸如对接机构,舱口或其他设备之类的特征的可伸缩刚性圆顶包括多个刚性弓形段,每个具有相对的端部分别在该特征的相对侧处被分开 围绕车辆的表面围绕围绕其相对端延伸的旋转轴线并通过延伸穿过该特征的弧形路径旋转运动。 段的径向尺寸交错,使得在圆顶的完全展开位置中,相邻的片段之间以最大相对角度彼此旋转,这些片段组合以在该特征上形成弓形屏蔽,并且 在圆顶的缩回位置,其中相邻的片段以相对于车辆的表面的共同角度一起旋转,这些片段彼此径向对准地嵌套。
    • 67. 发明授权
    • Radiation shielding device
    • 辐射屏蔽装置
    • US06239766B1
    • 2001-05-29
    • US08753846
    • 1996-12-02
    • Adrian David SmithPaul Clark
    • Adrian David SmithPaul Clark
    • H01Q152
    • H01Q1/526
    • The present invention relates to antennas. One of the problems which arises during operation of antenna arrangements is that spurious signals are emitted from mounting apertures and other surface features associated with a rearwardly facing ground plane, for instance, mounting bolts which couple some of the radiated energy, and through coaxial cable connector ports. The effect of all these unwanted signals is that they will couple with other radiating elements to form intermodulation products. In receive mode these intermodulation signals can severely impair the received signal quality. The present invention provides an antenna assembly comprising a support frame 52 and individually mounted layered antennas 56, wherein an insulator-conductor sheet such as a metallized plastics film 54 is interposed between the antennas and the support frame. There is also provided a method of manufacturing such a layered antenna and of receiving and transmitting signals by means of a layered antenna of this construction.
    • 本发明涉及天线。 在天线布置操作期间出现的问题之一是,寄生信号从安装孔和与向后的接地平面相关联的其它表面特征发射,例如安装螺栓,其耦合一些辐射能量,并通过同轴电缆连接器 港口。 所有这些不需要的信号的影响是它们将与其他辐射元件耦合以形成互调产物。 在接收模式下,这些互调信号可能严重损害接收到的信号质量。 本发明提供了一种天线组件,其包括支撑框架52和单独安装的分层天线56,其中诸如金属化塑料膜54之类的绝缘体导体片介于天线和支撑框架之间。 还提供了一种制造这样的层状天线的方法,并且通过这种结构的层状天线接收和发送信号。